AD/PZL/4 - Vertical Fin Rear Spar

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Legislation au F2006B06413 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


PZL M18 Dromader Series Aeroplanes

 

AD/PZL/4 Vertical Fin Rear Spar 13/95

Applicability: Model M18 aircraft with serial numbers up to and including 1Z013-25.

 

Requirement: 1. Inspect the vertical fin rear spar part number D33.100.00.0 for buckling and cracks using a light and mirror.

 

2. If buckling and cracking of the spar are found, replace the spar with a serviceable part.

 

Note: Transport Canada AD CF-95-09 refers.

 

Compliance: 1. Within 100 hours time in service after 7 December 1995, and thereafter at intervals not to exceed 12 calendar months.

 

2. Before further flight.

 

Background:  There is a possibility of cracking and deformation of the vertical fin rear spar. If not detected, this condition could lead to structural failure of the fin and seriously affect the controllability of the aircraft.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, are designed to maintain and enhance the safety of civil aviation operations within the country. Specifically, Part 39 - 105 of these regulations outlines the Civil Aviation Safety Authority's schedule of airworthiness directives, including AD/PZL/4, which pertains to the PZL M18 Dromader series aeroplanes. This directive addresses the identified risk of buckling and cracking in the vertical fin rear spar, which could compromise the aircraft's structural integrity and controllability if left unaddressed. The objective of this regulation is to ensure that aircraft maintain a high standard of airworthiness by requiring regular inspections and necessary repairs to the specified component to mitigate potential safety hazards. Compliance with these directives is mandatory, with inspections mandated within 100 hours after the directive's effective date and at intervals not exceeding 12 calendar months thereafter, as well as before further flight.

Scope and Application

The Civil Aviation Safety Authority (CASA) issues specific Airworthiness Directives (ADs) to ensure the safety of aircraft operations within Australia. AD/PZL/4 pertains to PZL M18 Dromader Series aeroplanes with serial numbers up to and including 1Z013-25. This directive requires regular inspections of the vertical fin rear spar part number D33.100.00.0 for signs of buckling and cracks using a light and mirror. If such defects are discovered, the spar must be replaced with a serviceable part. The requirement is for inspections to be conducted within 100 hours of time in service after 7 December 1995 and subsequently at intervals not exceeding 12 calendar months, as well as before further flight. This directive is integral to mitigating the risk of structural failure of the fin, which could compromise the controllability of the aircraft. The regulation applies across the Commonwealth of Australia, ensuring uniform safety standards are upheld by all relevant parties, including aircraft operators and maintenance personnel.

Key Provisions

The key provisions of the Civil Aviation Regulations 1998, Part 39 - 105, as outlined in AD/PZL/4, mandate specific maintenance and inspection requirements for PZL M18 Dromader Series Aeroplanes with serial numbers up to and including 1Z013-25. Section 39.105 requires the inspection of the vertical fin rear spar, specifically part number D33.100.00.0, to detect any signs of buckling and cracks using a light and mirror. If such defects are discovered, the regulation mandates the replacement of the spar with a serviceable part. This directive is cross-referenced with Transport Canada AD CF-95-09, indicating a coordinated approach to addressing this safety concern. Operators of the affected aircraft must adhere to stringent compliance timelines and conditions. Section 39.105 stipulates that the inspection must be conducted within 100 hours of time in service after 7 December 1995 and subsequently at intervals not exceeding 12 calendar months. Furthermore, the inspection must be performed before any further flight to ensure the continued airworthiness of the aircraft. These provisions aim to proactively identify and rectify structural issues that could compromise the safety and controllability of the aircraft. Failure to comply with the requirements outlined in Section 39.105 can lead to significant legal and operational consequences. The Civil Aviation Regulations impose penalties for non-compliance, which may include fines and potential grounding of the aircraft. The seriousness of the potential outcomes underscores the importance of adhering to the stipulated inspection and maintenance schedules. Non-compliance could also result in severe safety hazards, making it imperative for operators to follow the mandated procedures diligently. The potential for structural failure of the vertical fin rear spar, if left undetected, poses a serious risk to the controllability of the aircraft. Section 39.105 is designed to mitigate this risk by requiring regular and thorough inspections. The regulation's reference to Transport Canada AD CF-95-09 highlights the international collaboration in addressing common safety concerns across different jurisdictions. Operators must, therefore, ensure that they comply with these provisions to maintain the highest safety standards and avoid any adverse consequences.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.